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Tým NISA AIR

R22

BETA II

The two-seater R22 helicopter is a proven workhorse that has delivered excellent performance across various applications for over forty years. The R22 features a two-bladed rotor system that requires minimal hangar space, a T-shaped cyclic control for easy ingress and egress, and a crash-resistant fuel system. Its aluminum monocoque and steel tube structure with powder coating provide a lightweight yet robust airframe, while the aerodynamic fuselage optimizes airspeed and fuel efficiency. Powered by the reliable Lycoming O-360 engine, the R22 is tuned to deliver reserve power and enhanced performance at high altitudes and in hot weather conditions.

Thanks to its affordability and versatility, the R22 helicopter is used worldwide for flight training, livestock management, and personal transportation.

SPECIFICATIONS

Rating
Engine Lycoming O-540, six cylinder, carbureted
Horsepower Derated to 131 hp for takeoff and 124 continuous
Maximum Gross Weight 1370 lb (622 kg)
Approximate Empty Weight (including oil & standard avionics) 880 lb (399 kg)
Standard Fuel (16.9 gal) 101 lb (46 kg)
Auxiliary Fuel (9.4 gal) 56 lb (25 kg)
Pilot, Passengers, and Baggage (with standard fuel) 389 lb (176 kg)
Max Airspeed (Vne) 102 kts (189 km/h)
Cruise Speed up to 96 kts (178 km/h)
Maximum Range (no reserve) approx 250 nm (460 km)
Hover Ceiling IGE at 1370 lb 9400 ft
Hover Ceiling OGE at 1300 lb 8000 ft
Maximum Operating Altitude 14,000 ft
Electrical System 14 volt

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